EP 4152483 A1 20230322 - STRUCTURAL BATTERY FOR AN AIRCRAFT VEHICLE
Title (en)
STRUCTURAL BATTERY FOR AN AIRCRAFT VEHICLE
Title (de)
STRUKTURELLE BATTERIE FÜR EIN LUFTFAHRZEUG
Title (fr)
BATTERIE STRUCTURALE POUR UN VÉHICULE AÉRIEN
Publication
Application
Priority
US 202117405234 A 20210818
Abstract (en)
In one embodiment, systems and methods include using a battery (110) to provide electrical charge to a vehicle (100). The battery (110) comprises a first half of a housing (200) coupled comprising one or more air vents (206) and an anode (204) disposed at least partially within the first half of the housing (200). The battery (110) further comprises a second half of the housing (200) comprising one or more air vents (206), wherein the anode (204) extends from the first half of the housing (200) and into the second half of the housing (200). The battery (110) further comprises a pair of cathodes (302) disposed within the second half of the housing (200), wherein the pair of cathodes (302) extends from the second half of the housing (200) and into the first half of the housing (200), wherein the anode (204) is disposed between the pair of cathodes (302), wherein there is a gap (212) between the anode (204) and each one of the pair of cathodes (302).
IPC 8 full level
H01M 12/06 (2006.01); B60L 50/60 (2019.01); B60L 50/64 (2019.01); H01M 50/77 (2021.01); H01M 4/38 (2006.01); H01M 4/46 (2006.01); H01M 4/90 (2006.01); H01M 4/92 (2006.01)
CPC (source: EP KR US)
B60L 50/64 (2019.01 - EP); B60L 50/66 (2019.01 - EP); B60L 58/18 (2019.01 - EP); B64D 27/24 (2013.01 - KR US); H01M 4/463 (2013.01 - KR); H01M 4/466 (2013.01 - KR); H01M 12/02 (2013.01 - US); H01M 12/06 (2013.01 - KR); H01M 12/065 (2013.01 - EP); H01M 50/103 (2021.01 - US); H01M 50/107 (2021.01 - KR US); H01M 50/1537 (2021.01 - KR); H01M 50/183 (2021.01 - KR); H01M 50/249 (2021.01 - KR US); H01M 50/46 (2021.01 - KR); H01M 50/531 (2021.01 - KR); H01M 50/609 (2021.01 - US); H01M 50/618 (2021.01 - KR); H01M 50/627 (2021.01 - KR); H01M 50/673 (2021.01 - US); H01M 50/691 (2021.01 - KR US); H01M 50/77 (2021.01 - EP); B60L 2200/10 (2013.01 - EP); B64D 2221/00 (2013.01 - US); H01M 4/38 (2013.01 - EP); H01M 4/463 (2013.01 - EP); H01M 4/466 (2013.01 - EP); H01M 4/9016 (2013.01 - EP); H01M 4/9075 (2013.01 - EP); H01M 4/9083 (2013.01 - EP); H01M 4/926 (2013.01 - EP); H01M 2220/20 (2013.01 - EP US); H01M 2300/0065 (2013.01 - KR); H01M 2300/0085 (2013.01 - KR); Y02E 60/10 (2013.01 - EP); Y02T 50/60 (2013.01 - KR)
Citation (search report)
- [XAY] US 2004175603 A1 20040909 - YANG DE-QIAN [US], et al
- [A] JP 2017109553 A 20170622 - SHARP KK
- [A] CN 102088101 A 20110608 - GENIUS TOY TAIWAN CO LTD
- [Y] EP 3459842 A1 20190327 - BOEING CO [US]
- [Y] DE 102019218979 A1 20210610 - AIRBUS OPERATIONS GMBH [DE]
- [Y] CN 1538545 A 20041020 - LIU AOYU [CN]
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated extension state (EPC)
BA ME
Designated validation state (EPC)
KH MA MD TN
DOCDB simple family (publication)
EP 4152483 A1 20230322; JP 2023029291 A 20230303; KR 20230028160 A 20230228; TW 202310483 A 20230301; US 11705601 B2 20230718; US 2023054434 A1 20230223
DOCDB simple family (application)
EP 22188714 A 20220804; JP 2022129962 A 20220817; KR 20220101072 A 20220812; TW 111127988 A 20220726; US 202117405234 A 20210818